固体力学与飞行器总体设计

Z-pin增强树脂基复合材料单搭接连接性能

  • 董晓阳 ,
  • 李勇 ,
  • 张向阳 ,
  • 肖军 ,
  • 李吻
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  • 南京航空航天大学 材料科学与技术学院, 江苏 南京 210016
董晓阳男,硕士研究生。主要研究方向:先进复合材料三维增强技术。Tel:025-84892980E-mail:dongxiaoyang1112@163.com;李勇男,博士,教授,博士生导师。主要研究方向:先进复合材料自动化制造及工艺研究。Tel:025-84892980E-mail:lyong@nuaa.edu.cn

收稿日期: 2013-07-23

  修回日期: 2013-09-20

  网络出版日期: 2013-09-24

基金资助

军品配套项目(JPPT-1146)

Performance of Polymer Composite Single Lap Joints Reinforced by Z-pin

  • DONG Xiaoyang ,
  • LI Yong ,
  • ZHANG Xiangyang ,
  • XIAO Jun ,
  • LI Wen
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  • College of Materials Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received date: 2013-07-23

  Revised date: 2013-09-20

  Online published: 2013-09-24

Supported by

Military Product Item (JPPT-1146)

摘要

为提高复合材料单搭接头的连接性能,制备了不同参数的Z-pin增强单搭接头,通过拉伸试验,研究了Z-pin体积分数、直径以及植入角度对单搭接头连接性能的影响规律,分析了Z-pin对单搭接头性能的增强机理。结果表明Z-pin能明显提高复合材料单搭接头的连接性能:植入角度为90°、Z-pin直径为0.5 mm时,在0%~3.0%体积分数范围内,单搭接头强度随着Z-pin体积分数的增加呈线性增加,含3.0% Z-pin的接头剪切强度为16.76 MPa,比无Z-pin的接头强度提高了33.2%;Z-pin体积分数为1.5%、植入角度为90°时,Z-pin直径变化对单搭接头强度影响不大;含Z-pin体积分数为1.5%、直径为0.5 mm时,随着Z-pin植入角度(背离搭接末端)的增加,单搭接头强度先增加后下降,失效模式从Z-pin拔出失效转变为Z-pin剪断失效;在植入角度为40°时,剪切强度最大(21.04 MPa),比无Z-pin的接头剪切强度提高了67.1%。Z-pin植入角度(倾向于搭接末端)对单搭接头强度无影响。

本文引用格式

董晓阳 , 李勇 , 张向阳 , 肖军 , 李吻 . Z-pin增强树脂基复合材料单搭接连接性能[J]. 航空学报, 2014 , 35(5) : 1302 -1310 . DOI: 10.7527/S1000-6893.2013.0398

Abstract

To enhance the performance of polymer composite single lap joints, the joints reinforced with different configurations of Z-pins are manufactured and tested. The effects of the volume fraction, diameter and implant angles of the Z-pins on the strength of single lap joints are investigated and their reinforcing mechanism is also analyzed. The study finds that the Z-pin can improve the performance of single lap joints significantly: When the Z-pin's diameter is 0.5 mm and the implant angle is 90°, the joint's strength increases linearly with the Z-pin volume fraction from 0% to 3.0%. The maximum strength is 16.76 MPa with a 3.0% Z-pin fraction, which is 33.2% higher than that without Z-pin. It also reveals that the Z-pin's diameter has little influence on the strength of polymer composite single lap joints while the Z-pin fraction is 1.5% and the angle is 90°. The strength and failure model is strongly dominated by the implant angles of the Z-pin (against the joint edge) for a Z-pin fraction of 1.5% with a diameter of 0.5 mm. With the increase of the implant angles, the failure mode of the joint is transformed from Z-pin pulling out to Z-pin shearing. The strength reaches its peak value of 21.04 MPa at 40°, which is 67.1% higher than that without Z-pin. The implant angles of the Z-pin (along the joint edge) have no influence on its strength and failure mode.

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